Premium Information is available for this item - Upgrade for $1 a day
2520-01-498-8961
Vehicular Constant Velocity Drive Shaft Assembly
2520014988961 014988961 12409-3
An item designed to permit a greater degree of angle between two sections of a drive shaft, while transmitting rotary motion from the engine/transaxle assembly to the wheel hubs. The angle is split between the two joints working in a counterbalancing phase with input speed and output speed being identical. Includes items such as outboard and inboard joints, housing, protective bellows, shafts, mounting hardware and the like. The outboard universal joints turns with the wheel around a fixed center, while the inboard joint telescopes and turns at an angle sufficient to allow the required movement of the vehicle's suspension system. Excludes SHAFT, AXLE, AUTOMOTIVE; UNIVERSAL JOINT; UNIVERSAL JOINT, GEARED and PROPELLER SHAFT. View more Vehicular Constant Velocity Drive Shaft Assembly
May 2023
4
Marketplace 2520-01-498-8961
Request a Quotation from participating marketplace vendors
Related Documents 2520-01-498-8961 5+ Documents (More...)
2520014988961 014988961,12409-3 Account Upgrade 2520-01-498-8961Vehicular Constant Velocity Drive
Shaft Assembly2520014988961 014988961 12409-3 Upgrade your Account Upgrade 6685-00-082-1940Dial Indicating
2520014988961 014988961,12409-3 2520-01-498-8961 2520014988961 014988961 is an item designed to
2520014988961 014988961,12409-3 2520-01-498-8961 2520014988961 014988961 is an item designed to
www.nsnlookup.com /fsg-66/fsc-6685/us 6685-00-868-9845 Dial Indicating Pressure Gage 6685008689845 12409-3
(Active) Primary Buy RNCC 3 RNVC 2 DAC 5 12409-3 84147 - Andrew Llc (Active) Incomplete Secondary
Restrictions 2520-01-498-8961
2520-01-498-8961 is a Vehicular Constant Velocity Drive Shaft Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 2520-01-498-8961
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2520-01-498-8961
- US Air Force (FLL5)
- Effective Date:
- 1 Jul 2002
Approved Sources 2520-01-498-8961
- Part Number
- Manufacturer
- Status
- 12409-3
- Manufacturer
- 12867 - Gse Holdings Inc. (Replaced)
- Original Design
- Original Design
- 12409-3
- 0SMN2 - Itw Gse Inc. (Active)
- Advisory Reference
- Advisory Reference
Datasheet 2520-01-498-8961
- Characteristic
- Specifications
- FIIG
- Specifications
- A517T0
- Special Features [FEAT]
- Coupling Drive; Connects Deisel Engine And Pump; Part Of Refrigeration Unit Used To Cool Units On Plane
- End Item Identification [AGAV]
- F/A-22 Raptor
Management Data 2520-01-498-8961
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- FR
- F-22 AIRCRAFT
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - P
- Expendable. Reparable. Condemn at Intermediate. Stock Fund (except Munitions).
NATO Stock Numbers Related to 2520-01-498-8961
Freight Information 2520-01-498-8961
2520-01-498-8961 has freight characteristics.. 2520-01-498-8961 has a variance between NMFC and UFC when transported by rail and the description should be consulted.